Refer to the 1.914 dimension. B) What is its tolerance ? ________________________________ C) What is the MMC? (maximum material condition) ______________________________ D) What is the LMC(least material condition)? _______________________________

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Chapter1: Basic Modes Of Heat Transfer
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Problem 1.23P: Using the information in Problem 1.22, estimate the ambient air temperature that could cause...
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Refer to the 1.914 dimension.

B) What is its tolerance ? ________________________________
C) What is the MMC? (maximum material condition) ______________________________

D) What is the LMC(least material condition)? _______________________________

REVISIONS
DESCRIPTION
-PROPRIETARY-
THIS DOCUMENT AND DATA DISCLOSED
HEREIN OR HEREWITH IS NOT TO BE
REPRODUCED, USED, OR DISCLOSED
IN WHOLE OR IN PART TO ANYONE
WITHOUT THE PERMISSION OF
FLIR SYSTEMS INC.
ZONE LTR
DATE
APPROVED
NOTES:
1. INTERPRET DRAWING IAW MIL-STD-100.
2. INTERPRET DIMENSIONS AND TOLERANCES PER
ASME Y14.5-2009.
3. PART TO BE FREE OF BURRS AND SHARP EDGES.
O.001
VACUUM BAKE (10-4 TO 10 TORR). TEMP RISE
300 C/10 MIN TO 900 C. HOLD FOR 15
MIN AT 900 C. COOL TO 500 C IN 10 MIN,
500 C TO 100 C IN 30 MIN, REMOVE AND AIR
COOL TO ROOM TEMP (20 C).
2.125
A
.001 A
/5 THREAD RELIEF .10 LONG MAX.
2.059
6. IDENTIFY IAW MIL-STD-130 BY BAG
AND TAG INCLUDE LATEST REV LEVEL.
1.914-
/A ELECTROLESS NICKEL PLATE PER
MIL-C-26074, CL 2 (.0001/.0002 THK).
.867
8. DIMENSIONS TO APPLY AFTER FINISH.
9 GOLD PLATE INDICATED SURFACE PER
MIL-G-45204, TYPE_ I, GRADE A, CLASS
OPTIONAL, THICKNESS TO BE LESS THAN
.0005 PER SURFACE.
696
2X 45° X .010
- 45° X .015
ø1.274
ø.674
Ø.750 /9
+ø.028© AB
E.010 B
+ø.0280 AB
|+ 0.014@ A|
Ø.8740±.0005
I0.001 A
.875-40 UNS-2A
R.005 MAX -
Ø.107±.001 THRU
Uø.218 TO FULL
DIAMETER FAR SIDE ONLY
ø.028@ A B
PROJECT:
UNLESS OTHERWISE SPECIFIED
DIMENSIONS ARE IN INCHES
ALL DIMENSIONS IN [] ARE MM DRAWN
DO NOT SCALE DRAWING
FLIR
FLIR Systems Inc.
16505 sw 72nd Ave
Portland Or 97224
PROJECT
FRACTIONS + 1/32
DECIMALS XX 1.015
STRAIGHTNESS &/OR
FLATNESS: .005/IN
DATE
TITLE
G00'F XXX
THREADS:
SLEEVE
DEWAR
CHECK
HOLE
±.005 EXTERNAL-CLASS 2A
INTERNAL-CLASS 28
ANGLES,BENDS,&
INTERSECTIONS:90
PERPEND. I .003/IN MACHINED SURFACES:
Y OR BETTER
SAMPLES MUST BE APPROVED BY ENG.
XX
MATERIAL
REIMAGING
-.001
C00+ XXX
DESIGN
KOVAR
ANGLES O'30'
BENDS
FINISH
ENGR
DWG. NO.
REV
CONCEN. O.003/IN
64869
APPR
PRIOR TO STARTING PRODUCTION
CALC. WT.
SCALE 2:1
PRINTED:
SHEET 1 OF
Transcribed Image Text:REVISIONS DESCRIPTION -PROPRIETARY- THIS DOCUMENT AND DATA DISCLOSED HEREIN OR HEREWITH IS NOT TO BE REPRODUCED, USED, OR DISCLOSED IN WHOLE OR IN PART TO ANYONE WITHOUT THE PERMISSION OF FLIR SYSTEMS INC. ZONE LTR DATE APPROVED NOTES: 1. INTERPRET DRAWING IAW MIL-STD-100. 2. INTERPRET DIMENSIONS AND TOLERANCES PER ASME Y14.5-2009. 3. PART TO BE FREE OF BURRS AND SHARP EDGES. O.001 VACUUM BAKE (10-4 TO 10 TORR). TEMP RISE 300 C/10 MIN TO 900 C. HOLD FOR 15 MIN AT 900 C. COOL TO 500 C IN 10 MIN, 500 C TO 100 C IN 30 MIN, REMOVE AND AIR COOL TO ROOM TEMP (20 C). 2.125 A .001 A /5 THREAD RELIEF .10 LONG MAX. 2.059 6. IDENTIFY IAW MIL-STD-130 BY BAG AND TAG INCLUDE LATEST REV LEVEL. 1.914- /A ELECTROLESS NICKEL PLATE PER MIL-C-26074, CL 2 (.0001/.0002 THK). .867 8. DIMENSIONS TO APPLY AFTER FINISH. 9 GOLD PLATE INDICATED SURFACE PER MIL-G-45204, TYPE_ I, GRADE A, CLASS OPTIONAL, THICKNESS TO BE LESS THAN .0005 PER SURFACE. 696 2X 45° X .010 - 45° X .015 ø1.274 ø.674 Ø.750 /9 +ø.028© AB E.010 B +ø.0280 AB |+ 0.014@ A| Ø.8740±.0005 I0.001 A .875-40 UNS-2A R.005 MAX - Ø.107±.001 THRU Uø.218 TO FULL DIAMETER FAR SIDE ONLY ø.028@ A B PROJECT: UNLESS OTHERWISE SPECIFIED DIMENSIONS ARE IN INCHES ALL DIMENSIONS IN [] ARE MM DRAWN DO NOT SCALE DRAWING FLIR FLIR Systems Inc. 16505 sw 72nd Ave Portland Or 97224 PROJECT FRACTIONS + 1/32 DECIMALS XX 1.015 STRAIGHTNESS &/OR FLATNESS: .005/IN DATE TITLE G00'F XXX THREADS: SLEEVE DEWAR CHECK HOLE ±.005 EXTERNAL-CLASS 2A INTERNAL-CLASS 28 ANGLES,BENDS,& INTERSECTIONS:90 PERPEND. I .003/IN MACHINED SURFACES: Y OR BETTER SAMPLES MUST BE APPROVED BY ENG. XX MATERIAL REIMAGING -.001 C00+ XXX DESIGN KOVAR ANGLES O'30' BENDS FINISH ENGR DWG. NO. REV CONCEN. O.003/IN 64869 APPR PRIOR TO STARTING PRODUCTION CALC. WT. SCALE 2:1 PRINTED: SHEET 1 OF
Expert Solution
Step 1

Tolerance for the given dimension is 0.01. now as tolerance = upper limit - lower limit. and we also know the nominal dimension. So, MMC will be { nominal dimension + (tolerance/2)} and LMC will be { nominal dimension - (tolerance/2)}. So, 

MMC will be 1.919 and LMC will be 1.909.

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